Patent · US Active

Composite wing structure and methods of manufacture

US10639854B2 · kind B2 · utility

4Cited by
34References
15Claims
0Family size

Assignee

Inventors

Key dates

Filing dateFeb 3, 2017
Grant dateMay 5, 2020
Priority date
Expiry dateJan 9, 2038

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/40
  • WIPO fieldOther special machines
  • WIPO sectorMechanical engineering

Abstract

A method of manufacturing a tiltrotor wing structure including providing a spar mold having a plurality of bores extending from an exterior surface of the mold to an interior surface of the mold, the plurality of bores corresponding to a plurality of primary coordination holes in a spar member, the spar mold having a periphery defined by a top edge, a bottom edge and outboard ends; selecting a plurality of resin impregnated plies to ensure that the plies continuously extend beyond the periphery of the spar mold; laying the plies in the spar mold; curing the plies in the mold to form a cured spar member that extends beyond the periphery of the spar mold; and accurately drilling a plurality of primary coordination holes in the cured spar member in the spar mold using a tool positioned in the plurality of bores.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.